morgan state university m growing the future, leading the world or ce fluid mechanics ... · 2020....

7
Morgan State University “Growing the Future, Leading the World”CE FLUID MECHANICS RESEARCH LABORATORY Fracture Mechanics, Plasma Aerodynamics, Heavy Lift Morgan State University is embarking on cutting- edge research in the areas of heavy lift, fracture mechanics, plasma aerodynamics and super cavitation. As such, Morgan is fortunate to have approval for additional assets, such as subsonic and supersonic wind tunnels, with access to hypersonic wind tunnels located at the Department of Defense White Oak, Maryland Facility. Moreover, Morgan is a user of NASFRO, ANSYS, FLUENT, CFX and NASA OVERFLOW2. Finally, Morgan has past experience with NASTRAN. This lab will host research focusing on Fracture Mechanics (fracture growth and failure in airplane parts and materials), Plasma Aerodynamics (modeling and simulation), and Heavy Lift (space travel assistance) activities. Contact Information: CE Fluid Mechanics Research Laboratory ……………... Professor Arthur Willoughby [email protected] (443) 885-4238 FRACTURE MECHANICS Internal crack growth may inhibit the safe air travel of passengers in both the commercial and military sectors. Using NASGROW and ANSYS along with the Finite Element Modeling (FEM) Methodology fracture growth and failure analysis in airplane parts and materials was studied. The Boeing 787 Dreamliner was the identified aircraft to be researched against material abnormalities. Moreover, failure analysis plays a critical role in our transportation sector.

Upload: others

Post on 24-Oct-2020

2 views

Category:

Documents


0 download

TRANSCRIPT

  • Morgan State University “Growing the Future, Leading the World”™

    CE FLUID MECHANICS RESEARCH LABORATORY

    Fracture Mechanics, Plasma Aerodynamics, Heavy Lift

    Morgan State University is embarking on cutting-

    edge research in the areas of heavy lift, fracture mechanics,

    plasma aerodynamics and super cavitation. As such, Morgan

    is fortunate to have approval for additional assets, such as

    subsonic and supersonic wind tunnels, with access to

    hypersonic wind tunnels located at the Department of Defense

    White Oak, Maryland Facility. Moreover, Morgan is a user of

    NASFRO, ANSYS, FLUENT, CFX and NASA

    OVERFLOW2. Finally, Morgan has past experience with

    NASTRAN.

    This lab will host research focusing on Fracture

    Mechanics (fracture growth and failure in airplane parts and materials),

    Plasma Aerodynamics (modeling and simulation), and Heavy Lift (space travel assistance) activities.

    Contact Information:

    CE Fluid Mechanics Research Laboratory ……………... Professor Arthur Willoughby

    [email protected]

    (443) 885-4238

    FRACTURE MECHANICS

    Internal crack growth may inhibit the safe air travel of passengers in both the commercial

    and military sectors. Using NASGROW and ANSYS along with the Finite Element Modeling

    (FEM) Methodology fracture growth and failure analysis in airplane parts and materials was

    studied. The Boeing 787 Dreamliner was the identified aircraft to be researched against material

    abnormalities. Moreover, failure analysis plays a critical role in our transportation sector.

    Morgan State University “Growing the MorgM Morgan S

  • Morgan State University

    “Growing the Future, Leading the World”™

    CE Fluid Mechanics Research Laboratory

    PLASMA AERODYNAMICS

    Plasma Aerodynamics has a bright and promising in the aerodynamics area. Decrease in drag

    potentially 10–30% as well as creating invisible radar signature. Morgan State University is in the initial

    stages of modeling and simulation of this critical and revolutionary area. The European Space Agency and

    others have capitalized on the initial work done in Russia. Aircraft bodies immersed within a plasma field

    will increase lift-to-drag ratio, thus allowing a fuel cost saving within the transportation sector. Moreover,

    underwater supercavitation offers the same.

    HEAVY LIFT

    Morgan State University proposes and is actively seeking research in heavy lift to assist in space travel for

    the race back to the Moon. Morgan is a user of Satellite Tool Kit (STK) and ARcView-ARcInfo and can

    assist in trajectory plotting for this lunar mission. Heavy orbital lift becomes a major player for on-orbit

    travel and exploration.

    Morgan St

  • Morgan State University “Growing the Future, Leading the World”™

    CE Fluid Mechanics Research Laboratory

    Fluid Mechanics Instruments

    C6MKII Fluid Friction Measurement

    This is a unit for the detailed study of fluid friction head losses, which occur when an

    incompressible fluid flows through pipes, fittings and flow metering devices.

    S12 MKII Advanced Hydrology Study System

    Instructional Capabilities

    Determination of run-off hydrographs from model catchments, including multiple storms, moving storms, effect of reservoir storage and land drains

    Construction of draw-down curves for one- or two-well systems in a sand bed

    Hydraulic gradients in ground water flow Investigation of model stream flow in alluvial material

    Formation of river features and development over time

    Sediment transport, bed load motion, scour and erosion

    Morgan S

  • Morgan State University “Growing the Future, Leading the World”™

    CE Fluid Mechanics Research Laboratory

    S16 Hydraulic Flow Demonstrator

    The Armfield S16 Hydraulic Flow Demonstrator simply connects to a standard F1-10 Hydraulics

    Bench to permit the study of the following basic aspects of fluid flow:

    Closed conduit flow

    • Application of the Bernoulli and Continuity equations to converging and diverging flow

    • Effect of gradual and sudden changes in cross section (energy losses)

    • Using a contraction as a flow measuring device

    • Using a Pitot tube to measure velocity/velocity profile

    • Flow through a Culvert

    Open channel flow

    • Flow beneath an Undershot Weir (Sluice Gate)

    • Flow over Sharp Crested, Broad Crested and Ogee Weirs

    o Using hydraulic structures to measure flow in an open channel

    o Effect of changes in upstream and downstream water level

    o Characteristics of Clinging, Aerated, Depressed and Drowned Nappes

    • Sub-critical, Critical and Super-critical flow/depth. Changes in Specific Energy and control

    imposed by the minimum energy condition

    • Characteristics of Hydraulic Jumps

    o Force and energy conditions in a Hydraulic Jump

    o Flow patterns associated with Hydraulic Jumps

    • Flow over Drop Structures/Energy Dissipation

    • Changes in flow profile in relation to the Froude Number

    (predicting flow conditions in an open channel)

    • Observation of flow patterns associated with flow around hydraulic structures

    • Velocity of gravity waves in shallow water / Formation of surface waves near critical depth

    • Project work Evaluation of user constructed hydraulic structures

    MMoMorgan Sta

  • Morgan State University “Growing the Future, Leading the World”™

    CE Fluid Mechanics Research Laboratory

    FM62 Pelton Turbine

    This is a small-scale hydropower unit designed to demonstrate the operating principles of an

    impulse turbine.

    Instructional Capabilities

    Determining the characteristics of the turbine, including the relationships of volume flow rate,

    head, torque produced, power output and efficiency to rotational speed

    Comparison of throttle control and spear valve control of the speed of a Pelton Turbine

    Fluid Mechanics Laboratory (CBEIS 018)

    This lab will have research focusing on fracture mechanics (fracture growth and failure in airplane

    parts and materials), plasma aerodynamics (modeling and simulation), and heavy lift (space travel

    assistance) activities.

  • Morgan State University “Growing the Future, Leading the World”™

    CE Fluid Mechanics Research Laboratory

    F1-30 Flux Instructional Capabilities

    Measuring fluid density and relative density (specific gravity) of a liquid using a universal hydrometer

    Measuring fluid viscosity using a falling sphere viscometer

    Measuring fluid density and relative density (specific gravity) of a liquid using a pycnometer (density

    bottle)

    Observing the effect of capillary elevation between flat plates

    Measuring the effect of capillary elevation inside capillary tubes

    Verifying Archimedes principle using a brass bucket & cylinder with a lever balance

    Measuring atmospheric pressure using an aneroid barometer

    This apparatus introduces students to the following properties of fluids:

    Density and Relative Density (specific gravity)

    Viscosity Capillarity – capillary elevation between flat plates and in circular tubes

    Buoyancy (Archimedes’ principle)

    Atmospheric pressure

    The apparatus consists of a collection of components that demonstrate individual fluid properties. The

    components are stored on a common support frame manufactured from PVC with circular spirit level and

    adjustable feet for leveling. The apparatus is designed to stand on a suitable bench top, where some of the

    components can be operated independent from the support frame.

    A freestanding dual-scale lever balance is also supplied to support several of the demonstrations.

    MMorgan S

  • Morgan State University “Growing the Future, Leading the World”™

    CE Fluid Mechanics Research Laboratory

    This unit has been designed to demonstrate the hydraulic characteristics and settling efficiencies of

    a model settling basin. Although scale-up to industrial size sedimentation tanks is difficult, relevant

    deductions can be made as to how non-uniform flows occur and how these interact with the settling

    characteristics of particular suspensions.

    Demonstration Capabilities:

    Measuring flow short-circuiting and dead space using a tracer

    Comparison of real flow regimes with idealized flow models

    Effect of flow rate and baffle position on dispersion

    Measuring sediment removal efficiencies and relating these to the hydraulic characteristics

    S12 MKII Advanced Hydrology Study System